Shock/boundary layer interactions on oscillating airfoils are investigated using a high-order scheme and non linear turbulence models. The use of nonlinar models allows improving the numerical solution in terms of shock position and pressure coefficient distribution, as well as Reynolds stress level in the separated zone.
Numerical study of transonic shock/boundary layer interactions on an oscillating airfoil using a third-order scheme and nonlinear turbulence models
CINNELLA, Paola
2000-01-01
Abstract
Shock/boundary layer interactions on oscillating airfoils are investigated using a high-order scheme and non linear turbulence models. The use of nonlinar models allows improving the numerical solution in terms of shock position and pressure coefficient distribution, as well as Reynolds stress level in the separated zone.File in questo prodotto:
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